# Airbus Service Bulletin A330-25-3213

Copy: Revision 02 ("A330-25-3213 R02"), 74 pages: PDF https://openairdocs.org/files/sha256/85/b6/85b67503a3ce446f153be5c98d73a9f998b4d62405c73de63b2ace41fb970e53; text https://openairdocs.org/service-documents/airbus/a330-25-3213/file/85b67503a3ce.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2015-3631; AD 2016-25-31 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-25-3213
- Latest revision known: A330-25-3213, Revision 02, dated August 12, 2016 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/airbus/a330-25-3213

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2016-25-31](https://openairdocs.org/ad/2016-25-31.md), effective Feb 7, 2017: Revision 02

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-25-3213/proposed.md).

## Text (74 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2015-3631; AD 2016-25-31 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - P AX COMPARTMENT - MODIFY CDLS
WIRING LOOM IN UPPER COCKPIT DOOR PLATE COVER
MODIFICATION No.: 51911D44499
This page transmits Revision No.02 of Service Bulletin No.A330-25-3213
ADDITIONAL WORK
**CONF ALL
Additional work is required by this revision for aircraft modified by any previous issue of this Service
Bulletin.
AIRBUS recommends the additional work to be accomplished within one year after the issue of this
revision.
The additional work consists in:
- Replace the fasteners of the cover.
REASON
Revision No. 02 issued to incorporate changes found necessary and carried out during the
accomplishment of this Service Bulletin on aircraft with Manufacturer Serial Number (MSN) 0555, 0573
and 0587. An additional work added for aircraft modified by any previous revisions.
NOTE
: This revision satisfies the requirements of the subsequent Technical Adaptations (TA)
issued for the related MSN:
TA
 MSN
TA 80105052/013/2016
 0555, 0573 and 0587
CHANGES
The main changes of this revision are:
- Modification of the Kit 253213D02:
. 2 washers ASNA0113-56ADL replaced by NSA5379-3C
. 1 washer NAS1149CN949R replaced by NSA5379-3C
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
. 2 bolts NAS1096-3-14 replaced by MS21250-03006
. 1 cable tie NSA935401-03 added
- Introduction of the ADDITIONAL WORK, with the Kit COMPD01 and illustration BFAA created,
valid for aircraft modified by any previous issue
- Update of sentences in TEST paragraphs
- Revision of text and layout
- Addition of new sentence in ’ACCOMP LISHMENT INSTRUCTIONS’ paragraph.
NOTE
: Revised text and layout changes of this revision are not identified with revision bars.
SUMMARY
MODIFICATIONS
 Minor editorial or document structure change
 N
REASON/DESCRIPTION/OPERATIONAL
CONSEQUENCES
Minor editorial or document structure change
 N
GENERAL EVALUATION
 Minor editorial or document structure change
 N
MATERIAL PRICE INFORMATION
 Minor editorial or document structure change
 N
EFFECTIVITY
 Minor editorial or document structure change
 N
CONCURRENT REQUIREMENTS
 Minor editorial or document structure change
 N
REFERENCES / REPERCUSSIONS
 Minor editorial or document structure change
 N
NATURE OF THE WORK
 Minor editorial or document structure change
 N
MANPOWER
 Minor editorial or document structure change
 N
APPENDICES
 Minor editorial or document structure change
 N
Fig. A-GSAAA
 Minor editorial or document structure change
 N
Fig. A-GSAAA Sheet 01
 Minor editorial or document structure change
 N
PLANNING INFORMATION
EFFECTIVITY
 Minor editorial or document structure change
 N
Configuration definition
 Minor editorial or document structure change
 N
CONF 001
 Minor editorial or document structure change
 N
Material Effectivity
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
CONCURRENT REQUIREMENTS
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
REASON
 Minor editorial or document structure change
 N
History
 Minor editorial or document structure change
 N
Objective/Action
 Minor editorial or document structure change
 N
Advantages
 Minor editorial or document structure change
 N
Operational/Maintenance
Consequences
Minor editorial or document structure change
 N
DESCRIPTION
 Minor editorial or document structure change
 N
COMPLIANCE
 Minor editorial or document structure change
 N
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Classification
 Minor editorial or document structure change
 N
Accomplishment Timescale
 Minor editorial or document structure change
 N
APPROVAL
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
MANPOWER
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
WEIGHT AND BALANCE
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
ELECTRICAL LOAD DATA
 Minor editorial or document structure change
 N
REFERENCES
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
PUBLICATION AFFECTED
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
INTERCHANGEABILITY/MIXABILITY
 Minor editorial or document structure change
 N
Minor editorial or document structure change
 N
SPARES
 Minor editorial or document structure change
 N
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY
 Minor editorial or document structure change
 N
Procurement Addresses
 Minor editorial or document structure change
 N
Price and Availability
 Minor editorial or document structure change
 N
INDUSTRY SUPPORT INFORMATION
 Minor editorial or document structure change
 N
LIST OF COMPONENTS
 Minor editorial or document structure change
 N
Kit 253213D02R02
 Minor editorial or document structure change
 N
LIST OF MATERIALS - OPERATOR
SUPPLIED
Minor editorial or document structure change
 N
Consumable Materials
 Minor editorial or document structure change
 N
Consumable CMLD01
 Minor editorial or document structure change
 N
Components
 Minor editorial or document structure change
 N
Component COMPD01
 Minor editorial or document structure change
 N
Equipment
 Minor editorial or document structure change
 N
PARTS TO BE RE-IDENTIFIED BY
OPERATOR
Minor editorial or document structure change
 N
Reidentified part set REIDD01
 Minor editorial or document structure change
 N
TOOLING
 Minor editorial or document structure change
 N
ACCOMPLISHMENT INSTRUCTIONS
TASK 253213- 831-848-001-Modification
 Minor editorial or document structure change
 N
Task associated data - 001
 Minor editorial or document structure change
 N
Subtask 253213-910-201-001
 Minor editorial or document structure change
 N
Subtask 253213-900-202-001
 Minor editorial or document structure change
 N
Subtask 253213-941-201-001
 Minor editorial or document structure change
 N
Subtask 253213-862-201-001
 Minor editorial or document structure change
 N
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 253213-010-201-001
 Minor editorial or document structure change
 N
Subtask 253213-831-203-001
 Minor editorial or document structure change
 N
Subtask 253213-420-201-001
 Minor editorial or document structure change
 N
Subtask 253213-861-201-001
 Minor editorial or document structure change
 N
Subtask 253213-700-209-001
 Minor editorial or document structure change
 N
Subtask 253213-942-209-001
 Minor editorial or document structure change
 N
TASK 253213- 831-849-001-Modification -
Additional Work for Aircraft Modified by
Revision No. 01 or any Previous Issue
Minor editorial or document structure change
 N
Task associated data - 001
 Minor editorial or document structure change
 N
Subtask 253213-910-202-001
 Minor editorial or document structure change
 N
Subtask 253213-839-201-001
 Minor editorial or document structure change
 N
Subtask 253213-941-202-001
 Minor editorial or document structure change
 N
Subtask 253213-831-204-001
 Minor editorial or document structure change
 N
Subtask 253213-942-210-001
 Minor editorial or document structure change
 N
Fig. A-GBAAA
 Minor editorial or document structure change
 N
Fig. A-GBAAA Sheet 01
 Minor editorial or document structure change
 N
Fig. A-GBAAA Sheet 02
 Minor editorial or document structure change
 N
Fig. A-GBAAA Sheet 03
 Minor editorial or document structure change
 N
Fig. A-GBAAA Sheet 04
 Minor editorial or document structure change
 N
Fig. A-GBAAA Sheet 05
 Minor editorial or document structure change
 N
Fig. A-GBBAA
 Minor editorial or document structure change
 N
Fig. A-GBBAA Sheet 01
 Minor editorial or document structure change
 N
Fig. A-GBBAA Sheet 02
 Minor editorial or document structure change
 N
Fig. A-GBCAA
 Minor editorial or document structure change
 N
Fig. A-GBCAA Sheet 01
 Minor editorial or document structure change
 N
Fig. A-GBCAA Sheet 02
 Minor editorial or document structure change
 N
Fig. A-GBDAA
 Minor editorial or document structure change
 N
Fig. A-GBDAA Sheet 01
 Minor editorial or document structure change
 N
Fig. A-GBDAA Sheet 02
 Minor editorial or document structure change
 N
Fig. A-GBEAA
 Minor editorial or document structure change
 N
Fig. A-GBEAA Sheet 01
 Minor editorial or document structure change
 N
Fig. A-GBEAA Sheet 02
 Minor editorial or document structure change
 N
Fig. A-GBEAA Sheet 03
 Minor editorial or document structure change
 N
Fig. A-GBEAA Sheet 04
 Minor editorial or document structure change
 N
Fig. A-GBEAA Sheet 05
 Minor editorial or document structure change
 N
Fig. A-GBEAA Sheet 06
 Minor editorial or document structure change
 N
Fig. A-GBEAA Sheet 07
 Minor editorial or document structure change
 N
Fig. A-GBFAA
 Minor editorial or document structure change
 N
Fig. A-GBFAA Sheet 01
 Minor editorial or document structure change
 N
Fig. A-GBFAA Sheet 02
 Minor editorial or document structure change
 N
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 4
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Fig. A-GWAAA
 Minor editorial or document structure change
 N
Fig. A-GWAAA Sheet 01
 Minor editorial or document structure change
 N
Fig. A-GWBAA
 Minor editorial or document structure change
 N
Fig. A-GWBAA Sheet 01
 Minor editorial or document structure change
 N
FILING INSTRUCTIONS
This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS
Revision No. 01 was issued to add the removal/installation of the Anti Hijack Camera, update the
effectivity, add some covers to the parts to be re-identified and make some other minor changes.
NOTE
: This is only applicable for Revision No. 02 and subsequent. If information is required for
Revisions issued previous to this, please check your copies of Revision Transmittal
Sheets or contact AIRBUS.
REVISION SEQUENCE
ORIGINAL: Oct 12/04
REVISION No.: 01 - Apr 25/05
REVISION No. : 02 - Aug 12/16
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 5
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
This Page Intentionally Left Blank
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 6
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@A330
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
This summary is for information only and is not approved for modification of the aircraft.
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - P AX COMPARTMENT - MODIFY CDLS
WIRING LOOM IN UPPER COCKPIT DOOR PLATE COVER
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 None
MINOR
 51911D44499
NOTE
: As per EASA IR 21, a minor change is one that has no appreciable effect on the
mass, balance, structural strength, reliability, operational characteristics affecting the
airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
During the accomplishment of the Service Bulletin No. A340-25-4181 (EQUIPMENT/FURNISHINGS
- PASSENGER COMPARTMENT - INTRODUCE A MODIFIED INT RUSION AND PENETRATION
RESISTANCE COCKPIT DOOR), it was found that the electrical harness 7450VB, installed on the
cover of the upper cockpit door frame, is accessible from the cabin side. Therefore, the protection of
this harness must be improved.
This Service Bulletin introduces:
- a re-routing of the electrical harness 7450VB
- the installation of a protection plate for the electrical harness 7450VB.
This Service Bulletin has been validated on A340-600 aircraft MSN 0436.
Accomplishment of this Service Bulletin improves cockpit security by denying access to the electrical
harness from the cabin side.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 RECOMMENDED (1)
 CANCELS INSPECTION SB
 NO
POTENTIAL AD
 NO
 A/C OPERATION AFFECTED
 NO
RELIABILITY AFFECTED
 NO
 PAX COMFORT AFFECTED
 NO
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A330
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
COST SAVING
 NO
 ETOPS AFFECTED
 NO
STRUCTURAL LIFE EXTN
 NO
 VENDOR SB INVOLVED
 NO
NOTE
 (1)
: Service Bulletin recommended to be accomplished to prevent significant operational
disruptions.
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 253213D02R02
 1
 260.00
 Bolt, Washer, Screw, Wire protection,
Clamp, Nut, Cable Tie
Component COMPD01
 1
 See SB
 Bolt, Washer
EFFECTIVITY
This Service Bulletin is applicable to this (these) operator(s) :
38W 51X AAL ABD ACA ACI AEA AFR ALK ARG AZA AZU BEL
BER BGH CPA CRL CSA DAL DGA DLH EDW EIN F2I FWI G8E
GFA GIA GRL HDA HFY HVN KAL MAS MLM MOV OHY PLM QAF
QFA QTR RSY SAI SAS SXD TAE TAM TAP TCX THA THY TSC
UAE VKG WRC XAX XLF
CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the
following Service Bulletin(s):
Service Bulletin No. A330-25-3161
NOTE
: Service Bulletin No. A330-25-3161 (EQUIPMENT/FURNISHING - PASSENGER
COMPARTMENT - INTRODUCTION A MODIF IED INTRUSION AND PENETRATION
RESISTANCE COCKPIT DOOR) applies MOD 500014D44099.
REFERENCES / REPERCUSSIONS
TFU
 None
OEB
 None
AOT
 None
SIL
 None
ISI
 00.00.00198
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
NATURE OF THE WORK
AIRCRAFT
 YES
EQUIPMENT
 NO
HARD
 NO
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A330
SERVICE BULLETIN
SUMMARY
SOFT
 NO
OBRM
 NO
MANPOWER
Task 253213-831-848-001: Modification
TOTAL MANHOURS
 18.50
ELAPSED TIME (HOURS)
 14.00
Task 253213-831-849-001: Modification - Additional Work for Aircraft Modified by Revision No.
01 or any Previous Issue
TOTAL MANHOURS
 1.00
APPENDICES
None
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
FR16A
FR12
B
A
32MQ
31MQ
30MQ
25MQ−A
KEYPAD 25MQ
317LG
6296VS
6294VS
6295VS
A
32MQ
31MQ
30MQ
25MQ−A
KEYPAD 25MQ
317LG
6296VS
6294VS
6295VS
FR11
B
BEFORE
B
AFTER
Z220
40MQ40MQ
6297VS 6297VS
G_SB_253213_6_SAAA_01_00
Figure A-GSAAA - Sheet 01
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 4
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A330
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - P AX COMPARTMENT - MODIFY CDLS
WIRING LOOM IN UPPER COCKPIT DOOR PLATE COVER
MODIFICATION No.: 51911D44499
This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the
property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with
any information contained in it. It is delivered on the express condition that said document and the
information contained in it shall be treated as confidential, shall not be used for any purpose other than
that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall
not be duplicated in any manner (except for the purposes of performing the tasks described hereunder
and provided that any recipient of such document shall comply with the conditions herein), without
AIRBUS prior written consent.
1. PLANNING INFORMATION
**CONF ALL
A. EFFECTIVITY
(1) Models
330-202 330-203 330-223 330-243 330-301 330-303 330-321 330-322
330-323 330-341 330-342 330-343
(2) Effectivity by MSN
0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0065 0070-0072
0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116 0118
0120-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172
0177 0181 0195 0200 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238
0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269
0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303
0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334
0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370
0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401
0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441
0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473
0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0501
0503-0513 0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533
0535-0536 0539 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573
0576 0578-0579 0581 0584 0587-0588 0591 0597
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A330
SERVICE BULLETIN
(3) Effectivity by Operator
The Operator/MSN relationship is provided for information only and is correct at the time
of issue in accordance with the information available to AIRBUS. Any future changes
resulting from transfer of an aircraft from one operator to another will not be reflected in
this list unless the Service Bulletin is revised for another reason.
OPERATOR
 MSN
38W
 0401
51X
 0261
AAL
 0315 0323 0333 0337 0342 0370 0375 0380 0388
ABD
 0343
ACA
 0277 0279 0284 0344 0400 0408 0412 0419
ACI
 0507 0510
AEA
 0461 0505 0526 0551 0597
AFR
 0422 0443 0448 0458 0465 0481 0498 0500 0503 0516 0519 0567
0584
ALK
 0303 0306 0311 0313 0456
ARG
 0290 0300 0358 0364 0587
AZA
 0272 0339
AZU
 0462 0494 0527 0529 0532
BEL
 0030 0037 0045 0082 0095 0229 0249 0324
BER
 0288 0322 0403 0432 0444 0454 0469 0476 0493
BGH
 0255
CPA
 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539
0548 0565
CRL
 0285 0320
CSA
 0425
DAL
 0524 0533 0542 0549 0552 0578 0588 0591
DGA
 0240
DLH
 0570 0576 0579
EDW
 0291
EIN
 0269 0330 0397
F2I
 0087 0200
FWI
 0253
G8E
 0294 0299
GFA
 0276 0281 0286 0287 0334 0340
GIA
 0138 0140 0144 0148 0153 0165
GRL
 0230
HDA
 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405
0479 0512 0581
HFY
 0127 0211 0262
HVN
 0275 0366
KAL
 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350
0351 0368 0428 0484 0490 0550
MAS
 0116
MLM
 0451
MOV
 0535
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 13

@A330
SERVICE BULLETIN
OPERATOR
 MSN
OHY
 0072 0098 0143 0316 0345 0353 0362 0404 0437
PLM
 0265
QAF
 0487
QFA
 0506 0508 0513 0522 0553 0558 0564
QTR
 0441 0473 0489 0511 0521 0571
RSY
 0096 0120 0171
SAI
 0055 0070 0086
SAS
 0496 0497 0515 0568
SXD
 0530 0555 0573
TAE
 0348
TAM
 0232 0238 0247 0259 0361 0466 0472
TAP
 0181 0195 0223 0305 0308 0312 0317 0365 0372 0477 0486
TCX
 0254 0266 0301 0398
THA
 0050 0060 0062 0064 0065 0112 0122 0209 0224 0231 0346
THY
 0463 0504
TSC
 0111 0132 0177 0248 0250 0251 0271 0369 0407 0427 0480
UAE
 0283 0293 0295 0314 0326 0328 0382 0384 0392 0396 0409 0452
0455 0491 0509 0518 0525 0536
VKG
 0309 0349 0356 0357
WRC
 0296
XAX
 0054
XLF
 0501
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 14

@A330
SERVICE BULLETIN
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064
0065 0070 0071 0072 0082 0083 0086 0087 0095 0096 0098
0099 0102 0106 0109 0111 0112 0113 0116 0118 0120 0121
0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162
0165 0171 0172 0177 0181 0195 0200 0206 0209 0211 0219
0222 0223 0224 0226 0229 0230 0231 0232 0234 0238 0240
0241 0244 0247 0248 0249 0250 0251 0253 0254 0255 0256
0258 0259 0261 0262 0265 0266 0267 0269 0271 0272 0275
0276 0277 0279 0281 0283 0284 0285 0286 0287 0288 0290
0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306
0308 0309 0311 0312 0313 0314 0315 0316 0317 0320 0322
0323 0324 0326 0328 0330 0333 0334 0337 0338 0339 0340
0342 0343 0344 0345 0346 0348 0349 0350 0351 0353 0356
0357 0358 0361 0362 0364 0365 0366 0368 0369 0370 0372
0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397
0398 0400 0401 0403 0404 0405 0407 0408 0409 0412 0418
0419 0420 0421 0422 0423 0425 0427 0428 0432 0437 0439
0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461
0462 0463 0465 0466 0469 0472 0473 0476 0477 0479 0480
0481 0484 0486 0487 0489 0490 0491 0493 0494 0496 0497
0498 0500 0501 0503 0504 0505 0506 0507 0508 0509 0510
0511 0512 0513 0515 0516 0518 0519 0521 0522 0524 0525
0526 0527 0529 0530 0532 0533 0535 0536 0539 0542 0548
0549 0550 0551 0552 0553 0555 0558 0564 0565 0567 0568
0570 0571 0573 0576 0578 0579 0581 0584 0587 0588 0591
0597
001
(5) Configuration definition
**CONF 001
Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a
standard configuration.
(6) Material Effectivity
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 253213D02R02
 1
Consumable CMLD01
 1
Reidentified part set REIDD01
 1
Component COMPD01
 1
B. CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of
the following Service Bulletin(s):
Service Bulletin No. A330-25-3161
NOTE
: Service Bulletin No. A330-25-3161 (EQUIPMENT/FURNISHING -
PASSENGER COMPARTMENT - INTRODUCTION A MO DIFIED INTRUSION
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 4
6
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### Page 15

@A330
SERVICE BULLETIN
AND PENETRATION RESISTANCE COCKPIT DOOR) applies MOD
500014D44099.
C. REASON
(1) History
During the accomplishment of the Service Bulletin No. A340-25-4181
(EQUIPMENT/FURNISHINGS - PASSENGER COMPAR TMENT - INTRODUCE A
MODIFIED INTRUSION AND PENETRATION RESISTANCE COCKPIT DOOR), it was
found that the electrical harness 7450VB, installed on the cover of the upper cockpit
door frame, is accessible from the cabin side. Therefore, the protection of this harness
must be improved.
(2) Objective/Action
This Service Bulletin introduces:
- a re-routing of the electrical harness 7450VB
- the installation of a protection plate for the electrical harness 7450VB.
This Service Bulletin has been validated on A340-600 aircraft MSN 0436.
(3) Advantages
Accomplishment of this Service Bulletin improves cockpit security by denying access to
the electrical harness from the cabin side.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
Task 253213-831-848-001: Modification
(1) Removal the Electrical Harness 7450VB and the Cover of the Cockpit Door Frame
(2) Modify the Cover of the Cockpit Door Frame on Bench
(3) Install the Cover and the Electrical Harness 7450VB on the Cockpit Door Frame
Task 253213-831-849-001: Modification - Additional Work for Aircraft Modified by Revision
No. 01 or any Previous Issue
(1) Replace the Fasteners of the Cover
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 5
6
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### Page 16

@A330
SERVICE BULLETIN
E. COMPLIANCE
(1) Classification
RECOMMENDED: Service Bulletin recommended to be accomplished to prevent
significant operational disruptions.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin is recommended at the earliest opportunity
where manpower and facilities are available.
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organisation Approval No. EASA.21J.031.
If an aircraft listed in the effectivity has a modification or repair embodied that is not of
AIRBUS origin, and which affects the content of this Service Bulletin, the operator is
responsible for obtaining approval by its airworthiness authority for any adaptation necessary
before incorporation of the Service Bulletin.
G. MANPOWER
The manpower estimates given in this Service Bulletin are based on the direct labor cost to
do the work. These estimates assume that the work will be done by experienced personnel,
and may need to be revised upwards to suit operator’s circumstances. The estimates do not
include the time to prepare, plan or inspect the work. Manufacture and procurement of parts
and tools, drying times for paints, sealants, etc., and general administration work are also not
included.
Task 253213-831-848-001: Modification
Get Access
 3.50
On Aircraft
Removal the Electrical Harness 7450VB and the Cover
of the Cockpit Door Frame
3.00
Modify the Cover of the Cockpit Door Frame on Bench
 2.00
Install the Cover and the Electrical Harness 7450VB on
the Cockpit Door Frame
3.00
Tests
 3.00
Close-Up
 4.00
TOTAL MANHOURS
 18.50
ELAPSED TIME (HOURS)
 14.00
Task 253213-831-849-001: Modification - Additional Work for Aircraft Modified by Revision No.
01 or any Previous Issue
On Aircraft
Replace the Fasteners of the Cover
 1.00
TOTAL MANHOURS
 1.00
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 6
6
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### Page 17

@A330
SERVICE BULLETIN
H. WEIGHT AND BALANCE
The weight and balance estimates given in this Service Bulletin are based on the
Manufacturer’s Empty Weight (MEW) and do not include operator’s items. For the definition of
MEW and operator’s items, refer to Weight and Balance Manual (WBM) 01-00-07.
Manufacturers Empty Weight 0.401 KG (+0.8840 LB)
Effect on Balance 4.117 KGM (+29.778 LB.FT )
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
Aircraft Maintenance Manual (AMM)
 06-16-00 06-20-00 06-31-53
06-41-53 12-34-24 20-21-11
20-21-15 20-28-00 21-26-00
22-96-00 22-97-00 23-72-51
24-41-00 25-13-44 25-23-42
31-50-00 31-60-00 33-13-00
33-14-00 52-51-00
Consumable Material List (CML)
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-33-00 20-33-44 20-44-00
20-51-20 20-52-10 20-52-20
20-52-21 20-54-50 20-55-00
Service Bulletin (SB)
 A330-25-3161
A340-25-4181
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-42-00 51-44-00
Weight and Balance Manual (WBM)
 01-00-07
K. PUBLICATION AFFECTED
Aircraft Maintenance Manual (AMM)
 52-51-00 52-51-11 52-51-12
Aircraft Schematic Manual (ASM)
 52-51-00
Illustrated Parts Catalog (IPC)
 52-51-01
L. INTERCHANGEABILITY/MIXABILITY
The interchangeability/mixability possibilities are for new or modified parts introduced by the
accomplishment of this Service Bulletin.
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Cover
 F2527487100200
 F2528716800400
 03
 Not
Applicable
Cover
 F2527487100400
 F2528716800600
 03
 Not
Applicable
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 7
6
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### Page 18

@A330
SERVICE BULLETIN
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Cover
 F2527487100600
 F2528716800800
 03
 Not
Applicable
Cover
 F2527487101000
 F2528716801200
 03
 Not
Applicable
Cover
 F2527487101600
 F2528716801800
 03
 Not
Applicable
Cover
 F2527487101800
 F2528716802000
 03
 Not
Applicable
Cover
 F2527487102200
 F2528716802400
 03
 Not
Applicable
Cover
 F2527487102400
 F2528716802600
 03
 Not
Applicable
Cover
 F2527487102600
 F2528716802800
 03
 Not
Applicable
Cover
 F2527487102800
 F2528716803000
 03
 Not
Applicable
Cover
 F2527487103000
 F2528716803200
 03
 Not
Applicable
Cover
 F2527487103200
 F2528716803400
 03
 Not
Applicable
Cover
 F2527487103400
 F2528716803600
 03
 Not
Applicable
Cover
 F2527487103600
 F2528716803800
 03
 Not
Applicable
Cover
 F2527487104400
 F2528716804600
 03
 Not
Applicable
Cover
 F2527487104600
 F2528716804800
 03
 Not
Applicable
Cover
 F2527487104800
 F2528716805000
 03
 Not
Applicable
Cover
 F2527487105000
 F2528716805200
 03
 Not
Applicable
Cover
 F2527487105200
 F2528716805400
 03
 Not
Applicable
Cover
 F2527487105800
 F2528716806000
 03
 Not
Applicable
Cover
 F2527487600200
 F2528717000200
 03
 Not
Applicable
Cover
 F2527487601600
 F2528717001600
 03
 Not
Applicable
Cover
 F2527487603200
 F2528717003200
 03
 Not
Applicable
Cover
 F2527487604000
 F2528717004000
 03
 Not
Applicable
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 8
6
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### Page 19

@A330
SERVICE BULLETIN
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
Cover
 F2527487605000
 F2528717005000
 03
 Not
Applicable
Cover
 F2527487605800
 F2528717005800
 03
 Not
Applicable
Cover
 F2527487606000
 F2528717006000
 03
 Not
Applicable
Cover
 F2527487606200
 F2528717006200
 03
 Not
Applicable
Cover
 F2527487606400
 F2528717006400
 03
 Not
Applicable
Cover
 F2527487106400
 F2528717006400
 03
 Not
Applicable
Cover
 F2527487606600
 F2528717006600
 03
 Not
Applicable
Cover
 F2527487106600
 F2528717006600
 03
 Not
Applicable
Cover
 F2527487611200
 F2528717011200
 03
 Not
Applicable
Cover
 F2527487106800
 F2528717006800
 03
 Not
Applicable
Cover
 F2527487601800
 F2528717001800
 03
 Not
Applicable
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
M. SPARES
Cover F2527487100200
Cover F2527487100400
Cover F2527487100600
Cover F2527487101000
Cover F2527487101600
Cover F2527487101800
Cover F2527487102200
Cover F2527487102400
Cover F2527487102600
Cover F2527487102800
Cover F2527487103000
Cover F2527487103200
Cover F2527487103400
Cover F2527487103600
Cover F2527487104400
Cover F2527487104600
Cover F2527487104800
Cover F2527487105000
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 9
6
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### Page 20

@A330
SERVICE BULLETIN
Cover F2527487105200
Cover F2527487105800
Cover F2527487106400
Cover F2527487106600
Cover F2527487600200
Cover F2527487601600
Cover F2527487601800
Cover F2527487603200
Cover F2527487604000
Cover F2527487605000
Cover F2527487605800
Cover F2527487606000
Cover F2527487606200
Cover F2527487606400
Cover F2527487606600
Cover F2527487611200
The parts listed here must not be installed anymore on aircraft which have accomplished this
Service Bulletin or which have the equivalent production modification embodied.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 10
6
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### Page 21

@A330
SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Customers with aircraft shown in the effectivity of this Service Bulletin should send a
purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is :
Kit 253213D02R02
 AIRBUS Material, Logistics and Suppliers
ATP II B,
Hein-Sass-Weg 24
21129 HAMBURG
GERMANY
For ordering by internet:
http://spares.airbus.com
For ordering by E-mail: airbus.kit@airbus.com
Telephone Hotline:
+49 40 743 51616
(2) Price and Availability
Kit 253213D02R02
Cost
 260.00 USD
Availability
 90 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
B. INDUSTRY SUPPORT INFORMATION
AIRBUS will not provide industry support for accomplishment of this Service Bulletin.
C. LIST OF COMPONENTS
Kit 253213D02R02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
3
 NAS1833C08-370
 4
 INSERT
4
 MS21250-03012
 1
 BOLT
5
 NSA5379-3C
 3
 WASHER
6
 DAN125-4
 4
 WASHER
7
 NAS1102-08-6
 4
 SCREW
8
 F2527496220200
 1
 WIREPROT
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 11
6
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### Page 22

@A330
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
9
 MS21250-03006
 2
 BOLT
11
 MS21919WCH7
 4
 CLAMP
12
 NAS1096-2-10
 4
 SCREW
13
 MS21042L08
 4
 NUT
14
 NAS1149CN832R
 8
 WASHER
26
 NSA935401-03
 3
 TIE
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
Consumable CMLD01
ITEM
 DESCRIPTION
 REFERENCE TO CML
MAT. No.
QTY PER A/C
 SEE
NOTES
Epoxy Adhesive-- Legacy 2
 05EML8
 As required
Non Aqueous Cleaner-General
 08BAA9
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
(2) Components
Component COMPD01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
5
 NSA5379-3C
 3
 WASHER
9
 MS21250-03006
 2
 BOLT
NOTE
: If you find part numbers of hardware components in the related kit(s)
which you cannot identify in the LIST OF COMPONENTS of this Service
Bulletin, refer to Standards Manual (SM). The SM will give you the
correct part number to part number relationship.
NOTE
: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
NOTE
: The components listed above are only necessary if ADDITIONAL WORK
task is to be accomplished. The quantity of these items are to be ordered
as required.
(3) Equipment
None
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 12
6
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### Page 23

@A330
SERVICE BULLETIN
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
Reidentified part set REIDD01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
1
 F2528716800400
 COVER
 (1)
 F2527487100200
1
 F2528716800600
 COVER
 (1)
 F2527487100400
1
 F2528716800800
 COVER
 (1)
 F2527487100600
1
 F2528716801200
 COVER
 (1)
 F2527487101000
1
 F2528716801800
 COVER
 (1)
 F2527487101600
1
 F2528716802000
 COVER
 (1)
 F2527487101800
1
 F2528716802400
 COVER
 (1)
 F2527487102200
1
 F2528716802600
 COVER
 (1)
 F2527487102400
1
 F2528716802800
 COVER
 (1)
 F2527487102600
1
 F2528716803000
 COVER
 (1)
 F2527487102800
1
 F2528716803200
 COVER
 (1)
 F2527487103000
1
 F2528716803400
 COVER
 (1)
 F2527487103200
1
 F2528716803600
 COVER
 (1)
 F2527487103400
1
 F2528716803800
 COVER
 (1)
 F2527487103600
1
 F2528716804600
 COVER
 (1)
 F2527487104400
1
 F2528716804800
 COVER
 (1)
 F2527487104600
1
 F2528716805000
 COVER
 (1)
 F2527487104800
1
 F2528716805200
 COVER
 (1)
 F2527487105000
1
 F2528716805400
 COVER
 (1)
 F2527487105200
1
 F2528716806000
 COVER
 (1)
 F2527487105800
1
 F2528717000200
 COVER
 (1)
 F2527487600200
1
 F2528717001600
 COVER
 (1)
 F2527487601600
1
 F2528717001800
 COVER
 (1)
 F2527487601800
1
 F2528717003200
 COVER
 (1)
 F2527487603200
1
 F2528717004000
 COVER
 (1)
 F2527487604000
1
 F2528717005000
 COVER
 (1)
 F2527487605000
1
 F2528717005800
 COVER
 (1)
 F2527487605800
1
 F2528717006000
 COVER
 (1)
 F2527487606000
1
 F2528717006200
 COVER
 (1)
 F2527487606200
1
 F2528717006400
 COVER
 (1)
 F2527487106400
(1)
 F2527487606400
1
 F2528717006600
 COVER
 (1)
 F2527487106600
(1)
 F2527487606600
1
 F2528717006800
 COVER
 (1)
 F2527487106800
1
 F2528717011200
 COVER
 (1)
 F2527487611200
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 13
6
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@A330
SERVICE BULLETIN
F. TOOLING
None
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 14
6
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### Page 25

@A330
SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 253213-831-848-001 - Modification
WARNING
: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION
: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP
ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY
AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE
WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,
COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO
THIS:
- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS
NECESSARY ON WIRING AND COMPONENTS.
- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND
OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION
AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.
CAUTION
: BEFORE YOU DO WORK ON THE ELECTRICAL CIRCUIT AT THE REAR OF
A CIRCUIT BR EAKER PANEL, OPEN THE CIRCUIT BR EAKER 2XD(PANEL
721VU POSITION X5). THEN REMOVE THE CBMU FROM THE RACK. IF YOU
DO NOT OBEY THIS PRECAUTION, THERE IS A RISK OF DAMAGE TO THE
CBMU FROM UNWANTED VOLTAGE INJECTION.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has procedure accepted by the local authorities
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact Airbus for repair
instructions and approval.
NOTE
: Discarded parts must be managed at the operator’s discretion.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 15
6
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@A330
SERVICE BULLETIN
Task Associated Data
Zone
From 210 to 220
Modified FIN
317LG 7450VB
Access
Door
 831 841
Manpower
TOTAL MANHOURS
 18.50
ELAPSED TIME (HOURS)
 14.00
A. GENERAL
(1) Subtask 253213-910-201-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 06-16-00-912-801
06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
Task 20-21-15-912-801
Task 20-28-00-912-802
Consumable Material List (CML)
Elec. Std. Practices Manual (ESPM)
 20-33-00
20-33-44
20-51-20
20-52-10
20-54-50
Structural Repair Manual (SRM)
 51-42-00
51-44-00
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For identification of the zones, refer to AMM 06-20-00, Page Block 001.
(c) For identification of access panels, refer to AMM 06-41-53 Page Block 001.
(d) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to
Consumable Material List (CML).
(e) For circuit breaker safety practices, refer to AMM Task 06-16-00-912-801.
(f) For the general installation of electr ical wire harnesses, re fer to ESPM 20-33-00.
(g) Tag all the parts you must remove and retain to make the subsequent installation
easier.
(h) For the cable tie application and tooling, refer to ESPM 20-33-44.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 16
6
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@A330
SERVICE BULLETIN
(i) For the protection of the connectors , contacts and termi nals, refer to ESPM
20-54-50.
(j) Do a check of the electr ical connectors before you connect them, r efer to ESPM
20-52-10.
(k) Remove and install fasteners in accordance with SRM 51-42-00.
(l) To torque tighten the electrical component fasteners, refer to AMM Task
20-21-15-912-801.
(m) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.
(n) Put all the retained hardware in identified plastic bags and attach the bags to the
related unit.
(2) Subtask 253213-900-202-001 - Administrative
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
B. PREPARATION
(1) Subtask 253213-941-201-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-41-53, Page Block 001
Task 12-34-24-860-802
Task 23-72-51-000-801
Task 25-13-44-000-801
Task 25-23-42-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 17
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- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) If installed, remove the Anti Hijack Camera 12RA, refer to AMM Task
23-72-51-000-801.
(c) Remove the ceiling and sidewall panels 211MC, refer to AMM 06-41-53, Page
Block 001 and AMM Task 25-13-44-000-801.
(d) Remove the cover panels 221AC, refer to AMM 06-41-53, Page Block 001 and
AMM Task 25-23-42-000-801.
(e) In the cockpit, on the overhead panel, remove all the blanking plates necessary to
get access to the modification of the equipment and wiring.
(2) Subtask 253213-862-201-001 - De-Energize Electrical
Manpower Resources
Skills
 NON SPECIFIC
(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are
released:
- BAT 1, BAT 2, APU BAT,
- GEN 1, 2, APU GEN,
- EXT A (B).
(b) Open, safety/lock and tag these circuit breakers:
PANEL
 DESIGNATION
 FIN
 LOCATION
 SEE
NOTES
742VU
 701PP
 10PB1
 72 S
742VU
 702PP
 10PB2
 71 S
(c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to
operate the pushbutton switches on the overhead panel:
- 211VU (EMER ELEC PWR),
- 235VU (ELEC).
(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to
start the APU.
(e) Make sure that the external connector(s) is (are) not connected to the aircraft
receptacle(s) EXT PWR A (B).
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 18
6
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(f) Make sure that there is warning notice at the access door 121EL to tell persons not
to connect the external power connector(s).
C. PROCEDURE
(1) Subtask 253213-010-201-001 - Removal the Electrical Harness 7450VB and the
Cover of the Cockpit Door Frame
Work Zones and Access Panels
Zone
 Access/Work location
From
 210
 Access
 Door 831, Door 841
To
 220
Manpower Resources
Manhours
 3.00
Minimum number of person
 1
Subtask elapsed time
 3.00
Skills
 NON SPECIFIC
References
Elec. Std. Practices Manual (ESPM)
 20-33-00
Structural Repair Manual (SRM)
 51-42-00
Fig. A-GBAAA
Removal of the Electrical Harness
7450VB
Sheet 01
Sheet 02
Sheet 03
Sheet 04
Sheet 05
Fig. A-GWAAA
Wiring of the Electrical Harness 7450VB,
pre SB A330-25-3213
Sheet 01
Fig. A-GWBAA
Wiring of the Electrical Harness 7450VB,
post SB A330-25-3213
Sheet 01
Fig. A-GBCAA
Modification of the Cover of the Cockpit
Door Frame
Sheet 01
Sheet 02
Fig. A-GBBAA
Removal of the Cover from the Cockpit
Door Frame
Sheet 01
Sheet 02
(a) From the secure part, Item (28) of the RH cockpit door post, remove in accordance
with SRM 51-42-00 and as shown on Fig. A-GBAAA Sheet 04
 ,V i e wE :
1 Cover Item (20) Retain
and
2 Screw Item (21) Retain
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 19
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(b) Modify the wiring:
Refer to Fig. A-GBAAA Sheet 04
 , View F and ESPM 20-33-00
1
 Disconnect the plug 25MQA from the key pad 25MQ.
2
 From the plug 25MQA, remove:
1 Cable Tie Item (26) Discard
1 Plug Cover Item (27) Retain
2 Screw With Clamp Item (25) Retain
3
 Remove the wires of the electrical harness 7450VB, Item (2), from the plug
25MQA.
(c) From the RH cockpit door post, remove in accordance with SRM 51-42-00 and as
shown on Fig. A-GBAAA Sheet 02
 , Fig. A-GBAAA Sheet 03
 and Fig. A-GBAAA
Sheet 04
,V i e wG ,Ha n dJ :
1 Secure Part Item (28) Retain
1 Cover Plate Item (29) Retain
attached with:
6 Screw Item (30) Retain
5 Spacer Item (31) Retain
attached with:
10 Screw Item (32) Retain
6 Clamp Item (35) Retain
3 Clamp Item (36) Retain
9 Spacer Item (37) Retain
attached with:
9 Screw Item (33) Retain
9 Washer Item (34) Retain
NOTE
: Remove and retain the spacers, Item (37), if installed.
(d) Modify the wiring
Refer to ESPM 20-33-00.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 20
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1
 Disconnect the wires of the electrical harness 7450VB, Item (2), from the
release latches 30MQ, 31MQ and 32MQ as shown on Fig. A-GBAAA Sheet
01
 and Fig. A-GWAAA
.
2
 If installed, disconnect the electrical harness 7450VB from the circuit breaker
box 40MQ as shown on Fig. A-GBAAA Sheet 05
 , View L and Fig. A-GWBAA
.
(e) From the cover, Item (1), remove in accordance with SRM 51-42-00 and as shown
on Fig. A-GBAAA Sheet 02
 and Fig. A-GBAAA Sheet 05
 ,V i e wK :
FIN 317LG
1 Limit Switch Item (38) Retain
attached with:
2 Screw Item (39) Retain
As
required
Cable Tie Item (40) Discard
(f) Modify the wiring
Refer to ESPM 20-33-00
1
 Disconnect the wires of the electrical harness 7450VB from the Limit Switch
317LG, Item (38), as shown on Fig. A-GBAAA Sheet 05
 ,V i e wK .
2
 Remove the electrical harness 7450VB, Item (2), from the cover of the cockpit
door frame, Item (1), as shown on Fig. A-GBAAA Sheet 02
 , in accordance
with SRM 51-42-00:
(g) From the cockpit door frame, remove in accordance with SRM 51-42-00 and as
shown on Fig. A-GBBAA Sheet 02
 :
3 Cover Item (45) Retain
1 Cover Item (1) Retain
attached with:
1 Screw Item (41) Discard
1 Washer Item (43) Discard
and
2 Screw Item (42) Discard
2 Washer Item (44) Discard
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 21
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(h) From the cover, Item (1), remove as shown on Fig. A-GBCAA Sheet 01
 :
5 Cable Mount Item (46) Discard
(2) Subtask 253213-831-203-001 - Modify the Cover of the Cockpit Door Frame on
Bench
Manpower Resources
Manhours
 2.00
Minimum number of person
 1
Subtask elapsed time
 2.00
Skills
 NON SPECIFIC
Material necessary to do the job
Kit 253213D02R02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
3
 NAS1833C08-370
 4
 INSERT
Reidentified part set REIDD01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
1
 F2528716800400
 COVER
 (1)
 F2527487100200
1
 F2528716800600
 COVER
 (1)
 F2527487100400
1
 F2528716800800
 COVER
 (1)
 F2527487100600
1
 F2528716801200
 COVER
 (1)
 F2527487101000
1
 F2528716801800
 COVER
 (1)
 F2527487101600
1
 F2528716802000
 COVER
 (1)
 F2527487101800
1
 F2528716802400
 COVER
 (1)
 F2527487102200
1
 F2528716802600
 COVER
 (1)
 F2527487102400
1
 F2528716802800
 COVER
 (1)
 F2527487102600
1
 F2528716803000
 COVER
 (1)
 F2527487102800
1
 F2528716803200
 COVER
 (1)
 F2527487103000
1
 F2528716803400
 COVER
 (1)
 F2527487103200
1
 F2528716803600
 COVER
 (1)
 F2527487103400
1
 F2528716803800
 COVER
 (1)
 F2527487103600
1
 F2528716804600
 COVER
 (1)
 F2527487104400
1
 F2528716804800
 COVER
 (1)
 F2527487104600
1
 F2528716805000
 COVER
 (1)
 F2527487104800
1
 F2528716805200
 COVER
 (1)
 F2527487105000
1
 F2528716805400
 COVER
 (1)
 F2527487105200
1
 F2528716806000
 COVER
 (1)
 F2527487105800
1
 F2528717000200
 COVER
 (1)
 F2527487600200
1
 F2528717001600
 COVER
 (1)
 F2527487601600
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 22
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SERVICE BULLETIN
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
1
 F2528717001800
 COVER
 (1)
 F2527487601800
1
 F2528717003200
 COVER
 (1)
 F2527487603200
1
 F2528717004000
 COVER
 (1)
 F2527487604000
1
 F2528717005000
 COVER
 (1)
 F2527487605000
1
 F2528717005800
 COVER
 (1)
 F2527487605800
1
 F2528717006000
 COVER
 (1)
 F2527487606000
1
 F2528717006200
 COVER
 (1)
 F2527487606200
1
 F2528717006400
 COVER
 (1)
 F2527487106400
(1)
 F2527487606400
1
 F2528717006600
 COVER
 (1)
 F2527487106600
(1)
 F2527487606600
1
 F2528717006800
 COVER
 (1)
 F2527487106800
1
 F2528717011200
 COVER
 (1)
 F2527487611200
Consumable CMLD01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Epoxy Adhesive-- Legacy 2
 05EML8
Non Aqueous Cleaner-
General
08BAA9
Textile-Lint Free Cotton
 14SBA1
References
Structural Repair Manual (SRM)
 51-44-00
Fig. A-GBBAA
Removal of the Cover from the Cockpit
Door Frame
Sheet 01
Sheet 02
Fig. A-GBCAA
Modification of the Cover of the Cockpit
Door Frame
Sheet 01
Sheet 02
Fig. A-GBDAA
Installation of the Cover on the Cockpit
Door Frame
Sheet 01
Sheet 02
(a) Cut out the cable channels in the upper edge of the cover, Item (1), to the shape
that the electrical harness 7450VB can lead in a 90 degrees angle to the FWD
direction, as shown on Fig. A-GBCAA Sheet 02
 , View A and View B.
(b) Round the edges of the cable channel as shown Fig. A-GBCAA Sheet 02
 ,V i e wA
and View B.
(c) Drill four holes to the diameter of 14.5 mm (0.57 in.) in the upper edge of the cover,
Item (1), as shown on Fig. A-GBCAA Sheet 02
 , View C and Section A-A in
accordance with SRM 51-44-00.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 23
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(d) Deburr the holes in accordance with SRM 51-44-00 and clean the contact surfaces
with:
Textile-Lint Free
Cotton
14SBA1 As required
made moist with:
Non Aqueous
Cleaner-General
08BAA9 As required
(e) In the upper edge of the cover, Item (1), install, as shown on Fig. A-GBCAA Sheet
02
, View C and Section A-A:
4 Insert NAS1833C08-370 Item 3
with:
Epoxy Adhesive--
Legacy 2
05EML8 As required
(f) Re-identify the cover, Item (1):
1 Cover F2527487100200 Item (1)
becomes:
1 Cover F2528716800400 Item 1
or
1 Cover F2527487100400 Item (1)
becomes:
1 Cover F2528716800600 Item 1
or
1 Cover F2527487100600 Item (1)
becomes
1 Cover F2528716800800 Item 1
or
1 Cover F2527487101000 Item (1)
becomes:
1 Cover F2528716801200 Item 1
or
1 Cover F2527487101600 Item (1)
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 24
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SERVICE BULLETIN
becomes:
1 Cover F2528716801800 Item 1
or
1 Cover F2527487101800 Item (1)
becomes:
1 Cover F2528716802000 Item 1
or
1 Cover F2527487102200 Item (1)
becomes:
1 Cover F2528716802400 Item 1
or
1 Cover F2527487102400 Item (1)
becomes:
1 Cover F2528716802600 Item 1
or
1 Cover F2527487102600 Item (1)
becomes:
1 Cover F2528716802800 Item 1
or
1 Cover F2527487102800 Item (1)
becomes:
1 Cover F2528716803000 Item 1
or
1 Cover F2527487103000 Item (1)
becomes:
1 Cover F2528716803200 Item 1
or
1 Cover F2527487103200 Item (1)
becomes:
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 25
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@A330
SERVICE BULLETIN
1 Cover F2528716803400 Item 1
or
1 Cover F2527487103400 Item (1)
becomes:
1 Cover F2528716803600 Item 1
or
1 Cover F2527487103600 Item (1)
becomes:
1 Cover F2528716803800 Item 1
or
1 Cover F2527487104400 Item (1)
becomes:
1 Cover F2528716804600 Item 1
or
1 Cover F2527487104600 Item (1)
becomes:
1 Cover F2528716804800 Item 1
or
1 Cover F2527487104800 Item (1)
becomes:
1 Cover F2528716805000 Item 1
or
1 Cover F2527487105000 Item (1)
becomes:
1 Cover F2528716805200 Item 1
or
1 Cover F2527487105200 Item (1)
becomes:
1 Cover F2528716805400 Item 1
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 26
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or
1 Cover F2527487105800 Item (1)
becomes:
1 Cover F2528716806000 Item 1
or
1 Cover F2527487600200 Item (1)
becomes:
1 Cover F2528717000200 Item 1
or
1 Cover F2527487601600 Item (1)
becomes:
1 Cover F2528717001600 Item 1
or
1 Cover F2527487601800 Item (1)
becomes:
1 Cover F2528717001800 Item 1
or
1 Cover F2527487603200 Item (1)
becomes:
1 Cover F2528717003200 Item 1
or
1 Cover F2527487604000 Item (1)
becomes:
1 Cover F2528717004000 Item 1
or
1 Cover F2527487605000 Item (1)
becomes:
1 Cover F2528717005000 Item 1
or
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 27
6
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SERVICE BULLETIN
1 Cover F2527487605800 Item (1)
becomes:
1 Cover F2528717005800 Item 1
or
1 Cover F2527487606000 Item (1)
becomes:
1 Cover F2528717006000 Item 1
or
1 Cover F2527487606200 Item (1)
becomes:
1 Cover F2528717006200 Item 1
or
1 Cover F2527487606400 Item (1)
becomes:
1 Cover F2528717006400 Item 1
or
1 Cover F2527487606600 Item (1)
becomes:
1 Cover F2528717006600 Item 1
or
1 Cover F2527487611200 Item (1)
becomes:
1 Cover F2528717011200 Item 1
or
1 Cover F2527487106400 Item (1)
becomes:
1 Cover F2528717006400 Item 1
or
1 Cover F2527487106600 Item (1)
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 28
6
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### Page 39

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SERVICE BULLETIN
becomes:
1 Cover F2528717006600 Item 1
or
1 Cover F2527487106800 Item (1)
becomes:
1 Cover F2528717006800 Item 1
(3) Subtask 253213-420-201-001 - Install the Cover and the Electrical Harness 7450VB
on the Cockpit Door Frame
Work Zones and Access Panels
Zone
 Access/Work location
From
 210
 Access
 Door 831, Door 841
To
 220
Manpower Resources
Manhours
 3.00
Minimum number of person
 1
Subtask elapsed time
 3.00
Skills
 NON SPECIFIC
Material necessary to do the job
Kit 253213D02R02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
4
 MS21250-03012
 1
 BOLT
5
 NSA5379-3C
 3
 WASHER
6
 DAN125-4
 4
 WASHER
7
 NAS1102-08-6
 4
 SCREW
8
 F2527496220200
 1
 WIREPROT
9
 MS21250-03006
 2
 BOLT
11
 MS21919WCH7
 4
 CLAMP
12
 NAS1096-2-10
 4
 SCREW
13
 MS21042L08
 4
 NUT
14
 NAS1149CN832R
 8
 WASHER
26
 NSA935401-03
 3
 TIE
References
Aircraft Maintenance Manual (AMM)
 Task 20-21-11-911-801
Elec. Std. Practices Manual (ESPM)
 20-33-00
20-33-44
20-44-00
20-52-21
Structural Repair Manual (SRM)
 51-42-00
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 29
6
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### Page 40

@A330
SERVICE BULLETIN
References
Fig. A-GBDAA
Installation of the Cover on the Cockpit
Door Frame
Sheet 01
Sheet 02
Fig. A-GBEAA
Installation of the Electrical Harness
7450VB
Sheet 01
Sheet 02
Sheet 03
Sheet 04
Sheet 05
Sheet 06
Sheet 07
Fig. A-GWAAA
Wiring of the Electrical Harness 7450VB,
pre SB A330-25-3213
Sheet 01
Fig. A-GWBAA
Wiring of the Electrical Harness 7450VB,
post SB A330-25-3213
Sheet 01
(a) Install the re-identified cover, Item 1, in accordance with SRM 51-42-00 and as
shown on Fig. A-GBDAA Sheet 02
 ,w i t h :
2 Bolt MS21250-03006 Item 9
2 Washer NSA5379-3C Item 5
and
1 Screw MS21250-03012 Item 4
1 Washer NSA5379-3C Item 5
(b) Install on the cover, Item 1, in accordance with SRM 51-42-00 and as shown on
Fig. A-GBDAA Sheet 02
 :
3 Cover Item (45) Retained at
removal
(c) Lead the electrical harness 7450VB, Item (2), to the cover of the cockpit door frame
and the RH cockpit door post, as shown on Fig. A-GBEAA Sheet 02
 , and Fig. A-
GBEAA Sheet 07
,V i e wL .
(d) Connect the electrical harness 7450VB:
Refer to ESPM 20-33-00
1
 Connect the wires of the electrical harness 7450VB, Item (2), to the release
latches 30MQ, 31MQ and 32MQ, as shown on Fig. A-GBEAA Sheet 01
 , Fig.
A-GBEAA Sheet 03
 and on this Wiring Diagram, Fig. A-GWAAA
.
2
 If installed, connect the wires of the electrical harness 7450VB, Item (2), to the
circuit breaker box 40MQ as shown on Fig. A-GBEAA Sheet 04
 and on this
Wiring Diagram, Fig. A-GWBAA
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 30
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3
 Attach the wires, as shown on Fig. A-GBEAA Sheet 02
 , Fig. A-GBEAA Sheet
03
,V i e wD ,E ,Fa n dFig. A-GBEAA Sheet 04
 .
4
 Connect the wires of the electrical harness 7450VB, Item (2), to the limit
switch 317LG, Item (38), as shown on this Wiring Diagram, Fig. A-GWBAA
.
5
 Attach the additional wire length in a loop to the electrical harness 7450VB, as
shown on Fig. A-GBEAA Sheet 07
 ,V i e wL ,w i t h :
Refer to ESPM 20-33-44
2 Cable Tie NSA935401-03 Item 26
(e) Install on the cover, Item 1, in accordance with SRM 51-42-00 and as shown on
Fig. A-GBEAA Sheet 07
 ,V i e wL :
FIN 317LG
1 Limit Switch Item (38) Retained at
removal
attach with:
2 Screw Item (39) Retained at
removal
(f) Install on the RH cockpit door post, in accordance with SRM 51-42-00 and as
shown on Fig. A-GBEAA Sheet 02
 , Fig. A-GBEAA Sheet 03
 ,V i e wD ,E ,Fa n d Fig.
A-GBEAA Sheet 04
:
Refer to AMM Task 20-21-11-911-801
6 Clamp Item (35) Retained at
removal
3 Clamp Item (36) Retained at
removal
9 Spacer Item (37) Retained at
removal
attach with:
9 Screw Item (33) Retained at
removal
9 Washer Item (34) Retained at
removal
NOTE
: Install the spacers, Item (37), if retained at removal.
5 Spacer Item (31) Retained at
removal
attach with:
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 31
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10 Screw Item (32) Retained at
removal
1 Secure Part Item (28) Retained at
removal
1 Cover Plate Item (29) Retained at
removal
attach with:
6 Screw Item (30) Retained at
removal
NOTE
: Before you install the secure part, Item (38), and the cover plate,
Item (29), lead the wires of the key pad plug 25MQA through the
hole of the secure part and cover plate as shown on Fig. A-GBEAA
Sheet 06
,V i e wJ .
(g) To the plug 25MQA, connect the wires and install as shown on Fig. A-GBEAA
Sheet 06
,V i e wK :
Refer to ESPM 20-33-44
1 Plug Cover Item (27) Retained at
removal
2 Screw with clamps Item (25) Retained at
removal
1 Cable Tie NSA935401-03 Item 26
(h) Connect the plug 25MQA to the key pad 25MQ, refer t o ESPM 20-44-00.
(i) Install on the secure part of the RH cockpit door post, Item (28), in accordance with
SRM 51-42-00 and as shown on Fig. A-GBEAA Sheet 02
 and Fig. A-GBEAA Sheet
06
,V i e wJ :
1 Cover Item (20) Retained at
removal
attach with:
2 Screw Item (21) Retained at
removal
(j) Install on the cover, Item 1, in accordance with SRM 51-42-00 and as shown on
Fig. A-GBEAA Sheet 07
 ,V i e wLa n dN :
1 Wire Protection F2527496220200 Item 8
attach with:
4 Screw NAS1102-08-6 Item 7
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 32
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4 Washer DAN125-4 Item 6
4 Screw NAS1096-2-10 Item 12
8 Washer NAS1149CN832R Item 14
4 Clamp MS21919WCH7 Item 11
4 Nut MS21042L08 Item 13
(k) Do a continuity test of the modified electrical wires, refer to ESPM 20-52-21.
D. TEST
(1) Subtask 253213-861-201-001 - Energize Electrical Network
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 21-26-00-710-803
Task 22-96-00-740-801
Task 22-97-00-740-801
Task 24-41-00-861-801
Task 31-50-00-710-803
Task 31-50-00-740-801
Task 31-60-00-710-802
Task 33-13-00-710-801
Task 33-14-00-710-801
Elec. Std. Practices Manual (ESPM)
 20-52-20
(a) Job Set-up:
1
 In the cockpit, on the panel 235VU, push these pushbutton switches:
-G E N 1 , G E N 2 ,
- APU GEN (only if the A/C is energized from the external power).
2
 Remove the warning notices.
3
 Energize the aircraft electrical circuits, ref to AMM Task 24-41-00-861-801.
NOTE
: If the A/C is energized from the external power, make sure that
the pushbutton switches BAT 1, BAT 2, APU BAT and EXT A
(B) are pushed.
NOTE
: If the A/C is energized from APU, make sure that the
pushbutton switches BAT 1, BAT 2, APU BAT and APU GEN
are pushed.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 33
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4
 Remove the safety clips and/or tags and close/unlock tag these circuit
breakers:
PANEL
 DESIGNATION
 FIN
 LOCATION
 SEE
NOTES
742VU
 701PP
 10PB1
 72 S
742VU
 702PP
 10PB2
 71 S
(b) Preliminary Tests:
NOTE
: If the aircraft is operated in actual CAT III conditions, you must
also do the LAND CAT III capability test, refer to AMM Task
22-97-00-740-801
1
 On each connector which was disconnected:
- Do the checks as defined by ESPM 20-52-20.
NOTE
: The functional test and/or operational test requested by this
ESPM procedure is g iven hereafter.
2
 Do the Operational Test of the Instrument and Panel Integral Lighting, refer to
AMM Task 33-13-00-710-801.
3
 Do the Operational Test of Lights, refer to AMM Task 33-14-00-710-801.
4
 Do the Operational Test of the Avionics-Equipment Ventilation System, refer to
AMM Task 21-26-00-710-803.
5
 Do the Bite Test of the Auto Flight System (SYSTEM TEST), refer to AMM
Task 22-96-00-740-801.
6
 Do the Operational Test of the Electronic Centralized Aircraft Monitoring
(ECAM) Control Panel, refer to AMM Task 31-50-00-710-803.
7
 Do the test of the Flight Warning System (FWS), refer to AMM Task
31-50-00-740-801.
8
 Do the Operational Test of the Electronic Instrument System (EIS), refer to
AMM Task 31-60-00-710-802.
(2) Subtask 253213-700-209-001 - Test
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 52-51-00-710-801
Task 52-51-00-710-802
Task 52-51-00-710-803
Task 52-51-00-710-805
(a) Do the operational test of the Cockpit Door Lock System (CDLS), refer to AMM
Task 52-51-00-710-801.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 34
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(b) Do the operational test of the cockpit door routine access, refer to AMM Task
52-51-00-710-802.
(c) Do the operational test of the cockpit door emergency access, refer to AMM Task
52-51-00-710-803.
(d) Do the functional decompression test on the control box 24MQ, refer to AMM Task
52-51-00-710-805.
E. CLOSE-UP
(1) Subtask 253213-942-209-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 23-72-51-400-801
(a) Install the Anti Hijack Camera 12RA (if removed on SUBTASK 253213-941-201 001
Job Set-up ), refer to AMM Task 23-72-51-400-801.
(b) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(c) Remove the access platform(s).
(d) Put the aircraft back to its initial configuration.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 35
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This Page Intentionally Left Blank
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 36
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Task 253213-831-849-001 - Modification - Additional Work for Aircraft Modified by Revision
No. 01 or any Previous Issue
WARNING
: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION
: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP
ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY
AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE
WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,
COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO
THIS:
- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS
NECESSARY ON WIRING AND COMPONENTS.
- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND
OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION
AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has procedure accepted by the local authorities
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact Airbus for repair
instructions and approval.
NOTE
: Discarded parts must be managed at the operator’s discretion.
Task Associated Data
Zone
210
Manpower
TOTAL MANHOURS
 1.00
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 37
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A. GENERAL
(1) Subtask 253213-910-202-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
Structural Repair Manual (SRM)
 51-42-00, Page Block 001
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For identification of the zones, refer to AMM 06-20-00, Page Block 001.
(c) Remove and install fasteners, in accordance with SRM 51-42-00, Page Block 001.
(d) Put all retained hardware in identified plastic bags and attach the bags to the
related unit.
(2) Subtask 253213-839-201-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
B. PREPARATION
(1) Subtask 253213-941-202-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 38
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- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
C. PROCEDURE
(1) Subtask 253213-831-204-001 - Replace the Fasteners of the Cover
Work Zones and Access Panels
Zone
 Access/Work location
210
 Work location
 Frame 11
Manpower Resources
Manhours
 1.00
Minimum number of person
 1
Subtask elapsed time
 1.00
Skills
 NON SPECIFIC
Material necessary to do the job
Component COMPD01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
5
 NSA5379-3C
 3
 WASHER
9
 MS21250-03006
 2
 BOLT
NOTE
: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
NOTE
: The components listed above are only necessary if ADDITIONAL WORK
task is to be accomplished. The quantity of these items are to be ordered
as required.
References
Structural Repair Manual (SRM)
 51-42-00
Fig. A-GBFAA
Replacement of the Fasteners of the
Cover of the Cockpit Door Frame -
ADDITIONAL WORK
Sheet 01
Sheet 02
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 39
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(a) Remove, refer to Fig. A-GBFAA
:
1
 Remove from the cover, Item (1), in accordance with SRM 51-42-00 and as
shown on Fig. A-GBFAA Sheet 01
 ,v i e wAa n d Fig. A-GBFAA Sheet 02
 ,v i e w
B:
3 Cover Item (45) Retain
2 Screw Item (9) Discard
2 Washer Item (10) Discard
1 Screw Item (4) Retain
1 Washer Item (5) Discard
(b) Install, refer to Fig. A-GBFAA
:
1
 Install in the cover, Item (1), in accordance with SRM 51-42-00, as shown on
Fig. A-GBFAA Sheet 01
 ,v i e wAa n dFig. A-GBFAA Sheet 02
 ,v i e wB :
2 Bolt MS21250-03006 Item 9
2 Washer NSA5379-3C Item 5
1 Screw Item (4) Retained at
removal
1 Washer NSA5379-3C Item 5
2
 Install on the cover, Item (1), in accordance with SRM 51-42-00, as shown on
Fig. A-GBFAA Sheet 01
 ,v i e wAa n dFig. A-GBFAA Sheet 02
 ,v i e wB :
3 Cover Item (45) Retained at
removal
D. TEST
None
E. CLOSE-UP
(1) Subtask 253213-942-210-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
(a) Make sure that the work areas are clean and clear of tools and other items or
equipment.
(b) Put the aircraft back to its initial configuration.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 40
6
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**CONF ALL
FR16A
FR12
B
B
32MQ
31MQ
30MQ
25MQ−A
KEYPAD 25MQ
317LG
6296VS
6294VS
6295VS
FR11
A
C
A
Z220
40MQ
6297VS
1
1
NOTE:
INSTALLED AFTER ACCOMPLISHMENT
OF SERVICE BULLETIN A330−25−3215.
G_SB_253213_6_BAAA_01_00
Figure A-GBAAA - Sheet 01
Removal of the Electrical Harness 7450VB
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 41
6
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**CONF ALL
6296VS
6295VS
7450VB
G
G
G
G
G
E
D
C
J
J
J
H
H
6294VS
H
H
H
H
5128VN
TO 1181VC−A
5259VN
5199VN
(1)
(40)
(2)
(28)
(29)
(2)
7450VB
6297VS
40MQ
L
K
1
NOTE:
INSTALLED AFTER ACCOMPLISHMENT
OF SERVICE BULLETIN A330−25−3215.
1
(20)
G_SB_253213_6_BAAA_02_00
Figure A-GBAAA - Sheet 02
Removal of the Electrical Harness 7450VB
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 42
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SERVICE BULLETIN
**CONF ALL
(6 POS.)
D
(29)(28)
(30)
G_SB_253213_6_BAAA_03_00
Figure A-GBAAA - Sheet 03
Removal of the Electrical Harness 7450VB
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 43
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### Page 54

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SERVICE BULLETIN
**CONF ALL
E
25MQ−A
F
25MQ−A
F
(25)(25)
(20)
7450VB
(21) (26)
(27)
(2)(2)
G
7450VB
(2)
(31)
(32)
JH
(37)
(34)
(33)
(35)
(36)
2
2
NOTE:
REMOVE THE SPACER, ITEM (37), IF INSTALLED
(28)
VIEW H
VIEW J
G_SB_253213_6_BAAA_04_00
Figure A-GBAAA - Sheet 04
Removal of the Electrical Harness 7450VB
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 44
6
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SERVICE BULLETIN
**CONF ALL
40MQ
6297VS−B,D,F
L
(2)
K
317LG
(38)
(39)
1
NOTE:
INSTALLED AFTER ACCOMPLISHMENT
OF SERVICE BULLETIN A330−25−3215.
1
(1)
7450VB
G_SB_253213_6_BAAA_05_00
Figure A-GBAAA - Sheet 05
Removal of the Electrical Harness 7450VB
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 45
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**CONF ALL
FR16A
FR12
A
B
B
C
(1)
A
Z220
G_SB_253213_6_BBAA_01_00
Figure A-GBBAA - Sheet 01
Removal of the Cover from the Cockpit Door Frame
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 46
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**CONF ALL
C
(45)
(41)
(45)
(42)
(43)
(45)
(44)
(1)
G_SB_253213_6_BBAA_02_00
Figure A-GBBAA - Sheet 02
Removal of the Cover from the Cockpit Door Frame
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 47
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**CONF ALL
(1)
(46)
BEFORE
(1)
AFTER
A
B
C
G_SB_253213_6_BCAA_01_00
Figure A-GBCAA - Sheet 01
Modification of the Cover of the Cockpit Door Frame
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 48
6
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**CONF ALL
(0.51in.)
13.0mm
(0.35in.)
R 9.0mm
(0.50in.)
12.6mm
EDGES ROUNDED
EXISTING
DUCT
(0.24in.)
6.0mm
(0.56in.)
(14.3mm)
(0.20in.)
R 5.0mm
DUCT
EXISTING
A
B
(4.65in.)
118.0mm
(12.72in.)
323.0mm
(17.96in.)
458.0mm
(20.79in.)
528.0mm
(0.46in.)
11.6mm
A A
C
(0.57in.)
14.5mm DIA
(0.38in.)
9.5mm ADHESIVE
(MAT.NO.08−010A)
SECTION
AA
3
(1)
(1)
(1)
3 3 3
EDGES ROUNDED
G_SB_253213_6_BCAA_02_00
Figure A-GBCAA - Sheet 02
Modification of the Cover of the Cockpit Door Frame
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 49
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**CONF ALL
FR16A
FR12
A
B
B
C
(1)
A
Z220
G_SB_253213_6_BDAA_01_00
Figure A-GBDAA - Sheet 01
Installation of the Cover on the Cockpit Door Frame
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213
REVISION No.: 02 - Aug 12/16 Page: 50
6
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